Linear density triangular panel method is crashing when I'm trying to run it with thick wings

Questions, suggestions, feature requests, bug reports, feedbackCategory: QuestionsLinear density triangular panel method is crashing when I'm trying to run it with thick wings
Aaditya WangikarAaditya Wangikar asked 7 months ago

When I’m trying to run the aircraft with wings modelled as thick surface, then flow5 is crashing and shutting down. Can anyone help me try to resolve this issue?

André Deperroistechwinder Staff replied 7 months ago

Hello,
I can’t really say without having a look at the project file.
That being said, I strongly recommend to use uniform triangles which are far more robust numerically, offer the same precision, and have the benefit of smaller matrix size and reduced computation times.